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You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:F
[texts]Field of flow about a jet and effect of jets on stability of jet-propelled airplanes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003594028&ix=nu&I=0&V=D&pm=1
Keywords: Jet planes--Flight testing; Jet planes, Military; Aeronautics--Research; Downwash (Aerodynamics
Downloads: 109
[texts]Finite span wings in compressible flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 74
[texts]Flat plate cascades at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807842&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 83
[texts]Flat wing with sharp edges in a supersonic stream - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874043&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 168
[texts]Flight investigation at high mach numbers of several methods of measuring static pressure on an airplane wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613532&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Bombers; Aerodynamics--Research
Downloads: 110
[texts]Flight investigation at high speeds of flow conditions over an airplane wing as indicated by surface tufts - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613488&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Lift (Aerodynamics
Downloads: 110
[texts]Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613208&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Fighter planes; Aerodynamics--Research
Downloads: 107
[texts]Flight investigation of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613546&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Compressibility; Aerodynamics--Research
Downloads: 83
[texts]Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Control surfaces; Aerofoils; Aerodynamics--Research
Downloads: 105
[texts]Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805102&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 97
[texts]Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804734&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 128
[texts]Flight investigation of NACA Ds cowlings on the XP-42 airplane.:II,Low-inlet-velocity cowling with axial-flow fan and propeller cuffs - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805098&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Aerodynamics--Research
Downloads: 135
[texts]Flight investigation of wing-gun fairings on a fighter type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805073&ix=nu&I=0&V=D&pm=1
Keywords: Fire control (Aerial gunnery)--Equipment; Aerodynamics--Research
Downloads: 137
[texts]Flight measurements of airplane structural temperatures at supersonic speeds - Flight Research Center (U.S.
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834263&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Aerodynamics--Research
Downloads: 230
[texts]Flight measurements of the rudder control and sideslip characteristics of four vertical tail arrangements on the P-40 series airplanes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622095&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Steering-gear--Testing; Aerodynamics--Research
Downloads: 90
[texts]Flight measurements to determine effect of a spring-loaded tab on longitudinal stability of an airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003594145&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Stability of airplanes, Longitudinal; Aeronautics--Research
Downloads: 90
[texts]Flight studies of the horizontal-tail loads experienced by a modern pursuit airplane in abrupt maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613548&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 112
[texts]Flight tests of the lateral control characteristics of an F6F-3 airplane equipped with spring-tab ailerons - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605252&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 102
[texts]Flow of a compressible fluid past a circular arc profile - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003593774&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Compressibility; Aerodynamics
Downloads: 133
[texts]Flow of gas through turbine lattices - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807492&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 107
[texts]Flow of gases in narrow channels - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779980&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 96
[texts]Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 57
[texts]Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003610203&ix=nu&I=0&V=D&pm=1
Keywords: Guided bombs; Aerodynamics--Research
Downloads: 122
[texts]Formation of a vortex at the edge of a plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874042&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 76
[texts]Formulas for propellers in yaw and charts on the side-force derivative - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805575&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Yawing (Aerodynamics; Aeronautics--Research
Downloads: 141
[texts]Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854698&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 86
[texts]Frequency of occurrence of atmospheric gusts and of related loads on airplane structures - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808565&ix=nu&I=0&V=D&pm=1
Keywords: Airframes; Aerodynamics--Research
Downloads: 88
[texts]From linear mechanics to nonlinear mechanics - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874876&ix=nu&I=0&V=D&pm=1
Keywords: Remote control--Research; Nonlinear systems
Downloads: 111
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